View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 19649U 88102A 24357.64140187 .00000270 00000-0 16360-3 0 9998
2 19649 71.0014 62.6250 0003040 107.7123 252.4332 14.15065133862605
| Epoch (UTC): | 22 December 2024 15:23:37 |
| Eccentricity: | 0.0003040 |
| inclination: | 71.0014° |
| perigee height: | 840 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 62.6250° |
| argument of perigee: | 107.7123° |
| revolutions per day: | 14.15065133 |
| mean anomaly at epoch: | 252.4332° |
| orbit number at epoch: | 86260 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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